A high energy catapult assembly may comprise an outer tube and an inner tube located within the outer tube. The outer tube may be configured to telescope relative to the inner tube. A propellant cartridge may be located in an inner tube chamber of the inner tube. An actuator may be configured to change an open volume of the inner tube chamber.


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    Titel :

    VARIABLE VOLUME HIGH ENERGY CATAPULT ASSEMBLIES FOR EJECTION SYSTEMS


    Beteiligte:
    SALOIS MATTHEW D (Autor:in) / BENJAMIN JEFF (Autor:in) / MUELLER KEVIN (Autor:in)

    Erscheinungsdatum :

    20.10.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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